SpaceAtlas Space Object Data
NASA JPL SBDB · 2017 UJ2

2017 UJ2

2017 UJ2 belongs to the Apollo group of near-Earth asteroids, whose orbits cross the path of Earth; with a semi-major axis of 1.116 AU it takes 1.18 yr to circle the Sun.

Apollo Observations: 27
Orbital Period · P
1.18 yr
v(q)
33.9 km/s
v(Q)
23.5 km/s
TJ
5.57
Eccentricity · e
0.182

Orbit and dynamics

Between its closest point (0.913 AU) and its farthest (1.319 AU), the heliocentric distance changes by 0.406 AU over every revolution.

One full revolution takes 1.18 yr (431 days), computed from the semi-major axis of 1.116 AU.

An eccentricity of 0.182 makes the orbit moderately elongated.

Its inclination of 0.48° keeps it close to the plane of the ecliptic.

By the vis-viva equation its orbital speed rises to 33.9 km/s at perihelion and falls to 23.5 km/s at aphelion.

Because q < 1 AU and Q > 1 AU, this orbit geometrically intersects the region of Earth's orbit.

Size and surface

Neither a measured diameter nor a reliable absolute magnitude is available for 2017 UJ2, so its physical size remains unconstrained.

Observation record and orbit quality

Astrometry from 27 individual observations underpins this orbit; the fit leaves an RMS residual of 0.4631 arcseconds.

Condition code U = 5 indicates a moderately constrained orbit; predictions decades ahead still carry noticeable uncertainty.

About these computed values

Orbital periods, perihelion and aphelion speeds, and diameter estimates on this page are computed by SpaceAtlas from the JPL SBDB orbital elements. They are derived quantities, not values copied from the source catalogue.

Orbital Parameters

Semi-Major Axis
1.116 AU
Eccentricity
0.182
Perihelion
0.913 AU
Aphelion
1.319112 AU
Inclination
0.48°
Orbital Period
— yr
Epoch
2461200.5
Mean Anomaly
146.1°

Orbit diagram

The Sun sits at the focus (orange). Earth's orbit is the grey circle at 1 AU. The red dot marks the object's position at the catalog epoch.

3D orbit (interactive)

Drag to rotate; scroll or pinch to zoom. The Sun is at the focus (orange), Earth's orbit is the grey ring at 1 AU, and the red dot marks the object's current position.

Close approaches

Predicted close approaches to Earth, from NASA's Center for Near-Earth Object Studies (CNEOS).

Date (UTC)Miss distanceVelocity
2030-Mar-20 15:49 0.275796 AU
41258480 km
5.88 km/s
2030-Oct-29 10:29 0.002250 AU
336549 km
7.35 km/s
2036-May-27 06:05 0.100030 AU
14964334 km
10.16 km/s
2037-Jan-22 06:39 0.304492 AU
45551317 km
6.42 km/s
2043-Apr-05 16:32 0.245634 AU
36746295 km
5.13 km/s
2049-May-16 22:22 0.283619 AU
42428779 km
16.02 km/s
2050-Feb-14 08:48 0.325760 AU
48733018 km
6.68 km/s
2050-Nov-13 07:56 0.251277 AU
37590565 km
16.23 km/s

Distances in astronomical units (AU) and kilometres. Source: NASA/JPL CNEOS Close Approach Data API.

Physical Parameters

Diameter
— km
Albedo
—
Density
— g/cm³
Rotation Period
— h
Absolute Magnitude
30.9

Orbit Quality

RMS
0.46313
Condition
5
Orbit ID
—
Data source: NASA JPL Small-Body Database · NASA CNEOS. Orbital periods, perihelion and aphelion speeds, and diameter estimates on this page are computed by SpaceAtlas from the JPL SBDB orbital elements. They are derived quantities, not values copied from the source catalogue.

Keep exploring

Explore asteroids, comets and near-Earth objects with JPL orbital data.